AD/PA-32/10 - Fuel System Improvements - Modification
1AD/PA-32/10 - Fuel System Improvements - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-32/10 - Fuel System Improvements - Modification.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/10 Fuel System Improvements - Modification 12/67
Applicability: Model PA-32-260 with S/Nos. 32-1 to 32-14, 32-16 to 32-853; Model PA-32-300
with S/Nos. 32-15 and 32-40001 to 32-40153.
Document: 1. Piper SB Nos. 249 and 253; or
- FAA AD 67-26-2.
Compliance: Within 100 hours time in service after 22 February 1968.